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Induced-Drag Calculations in the Unsteady Vortex Lattice Method (2013)

First Author: Simpson R

Attributed to: Nonlinear Flexibility Effects on Flight Dynamics and Control of Next-Generation Aircraft funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.2514/1.j052136

Publication URI: http://dx.doi.org/10.2514/1.j052136

Type: Journal Article/Review

Parent Publication: AIAA Journal

Issue: 7